Choice of the rational scheme of load-caring frames of integral arrangement fighter
Aviation technics and technology
Аuthors
*, **Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
*e-mail: amidvoryalots@mail.ru
**e-mail: design101@mai.ru
Abstract
This article considers the method of strength and parametric analysis for the perfection of frames designs for the tail part fuselage frame of the integral composition fighter. An object of analysis is the structure of a full-size power with a ring in pod zone of the integral composition fighter two diverse engines. It is consider the causing of form of cross-section fuselage section to rational scheme of load-caring frames.Keywords:
design; frame; load; strength; parameters; mass.Download